Rolls-Royce RB211-524D419
Service difficulty reports · 92
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'RB211524D419' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'RB211524D419' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2020FA0000021Actuator · failedWE EXPERIENCED A FAILURE OF THE RH BODY LANDING GEAR DOOR ACTUATOR IN FLIGHT WHICH CAUSED THE RELEASE OF NR 1 SYSTEM HYDRAULIC FLUID. THE ACTUATOR FAILED AT THE END CAP/GLAND NUT THAT HOUSES THE SEAL FOR THE RAM. THE BREAK OF THE END CAP IS FROM SAFETY WIRE SDR 0126200801Engine · malfunctionedON TAKEOFF ROLL, NR 3 ENGINE N2 WENT TO 114 PERCENT FOR LESS THAN 2 SECONDS, EPR WAS 1.4, ALL OTHER ENGINE GAGES NORMAL, AIRSPEED WAS 70 KTS. ABORTED TO, RETURNED TO RAMP.SDR 0331200702Engine · bird ingestionAT ROTATION NR 2 ENG VIB ANNUNICATOR LIGHT & ENG VIB LIGHT FOR NR 2 ENG ILLUM, ACCOMPANIED BY VIB & ABNORMAL SOUND. NR 2 ENG SECURED IAW CHECKLIST, NO VIB NOTED AFTER SHUTDOWN. FUEL JETTISON, ACFT RETURNED WITHOUT FURTHER INCIDENTS. ON POSTFLIGHT INSPECTIOSDR 1023200603Warning Light · illuminatedON DEPARTURE (GYD), JUST AFTER V1, NR 1 ENGINE VIBE LIGHT ILLUMINATED, VIBE METER NR 1 OFF SCALE HIGH, INCLUDING VIBRATION AS WELL. ENGINE SHUT DOWN, FUEL DUMP, AND RETURNED TO (GYD).CORRECTIVE ACTIONS, PENDING.SDR 1017200602Engine · power lossDURING CLIMB FROM (ELLX) AT AROUND FL 180 FT, NR 1 THROTTLE IS AT FORWARD STOP TO MAINTAIN CLIMB THRUST. IN CRUISE NR 1 THROTTLE IS AT 1.5 UNITS - (4) KNOBS AHEAD OF ENGINES 2, 3, 4. NOTE ALL ENGINE PARAMETERS NORMAL AT LOW ALT, BELOW 189 THROTTLE POSITIONS SDR 0925200603Compressor · stalledDURING TO ROLL (SKBO), APPROX. 125 KTS., NR 4 ENGINE COMPRESSOR STALLED - ABORTED TO, RETURN TO GATE. FINDINGS - CORRECTIVE ACTIONS - TBD.SDR 0808200601Engine · noneON TAKEOFF AT SGES (AGT), NR 3 ENGINE BEGAN TO VIBRATE AND AMBER ENGINE VIB LIGHT CAME ON. ENGINE SHUTDOWN AND PROCEDURE TO COMPLETE THE HIGH ENGINE VIBRATION RB211 CHECKLIST. DISCREPANCY DUE TO BIRDSTRIKE/INJESTION. PERFORMED CONDITIONAL ENGINE BIRDSTRIKE SDR AU510001639Frame · scratched(AUS) FORWARD PRESSURE BULKHEAD AFT FACE OUTER CHORD SCRATCHED IN BEND RADIUS LOCATED AT LBL46/WL235 AND RBL24/WL268. SUSPECT A SHARP OBJECT WAS USED TO REMOVE SEALANT. FOUND DURING INSPECTION IAW AD/B747/159. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA NSDR AU510002178Panel · missing(AUS) NR 4 ENGINE VIGV ACCESS PANEL MISSING. INVESTIGATION ALSO FOUND THE LP COMPRESSOR ACOUSTIC LINING DAMAGED AT THE 6 O`CLOCK POSITION WITH A HOLE APPROXIMATELY 150MM BY 100MM (6IN BY 4IN) IN THE SKIN. VIGV CONTROLLER PANEL SUPPORT STRUCTURE ALSO DAMAGED. (SDR AUS20040443Indicator · faulty(AUS) LT OB TRAILING EDGE FLAP INDICATOR FAILED.SDR AUS20040390Bolt · incorrect(AUS) LT WING LANDING GEAR TO LANDING GEAR DOOR TIE ROD BOLTS INCORRECTLY FITTED. BOLTS WERE FITTED UPSIDE DOWN. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040127Blanket · deteriorated(AUS) APU DUCT INSULATION BLANKET BURNED AND IN POOR CONDITION.SDR AUS20031255Ballast · failed(AUS) LIGHTING BALLAST LOCATED AT SEAT 19JK FAILED.SDR AUS20031205Wire Harness · worn(AUS) WIRING LOOM LOCATED AT BS 1000 BEHIND OVERHEAD LOCKERS CHAFED THROUGH INSULATION BLANKET AND CONTACTED FUSELAGE FRAME CAUSING BURNING OF WIRES AND DAMAGE TO THE INSULATION BLANKET AND FRAME. AREA OF DAMAGE TO FRAME WAS APPROXIMATELY 4.762MM BY 2.381MM(0.SDR AUS20030882Tire · failed(AUS) NR 5F TIRE TREAD SEPARATED FROM CASING. TIRE REMAINED INFLATED. NIL DAMAGE EVIDENT TO REST OF AIRCRAFT. SUSPECT CAUSED BY FAILURE OF TREAD TO BOND TO CASING DURING RETREAD.SDR AUS20030634Slide · failed(AUS) DOOR NR 1 RT SLIDE RAFT FAILED.SDR AUS20030518Radio · failed(AUS) DUAL HF SYSTEM FAILURE. ON ARRIVAL IT WAS REPORTED THAT NR 1 HF SYSTEM WANDERS OFF FREQUENCY AND BECOMES GARBLED. NR 2 HF WOULD NOT TUNE TO THE FREQUENCY SELECTED. THE NR 1 SYSTEM WAS RE-RACKED AND OPERATED NORMALLY. THE NR 2 SYSTEM TRANSCEIVER AND COUPSDR AUS20021287Stator · disintegrated(AUS) NR 4F BRAKE STATOR DISINTEGRATED CAUSING DAMAGE TO WHEEL.SDR AUS20021270Tie Rod · broken(AUS) NR 3 ENGINE EXPERIENCED HIGH VIBRATION LEVELS. INSPECTION FOUND A NACELLE TIE ROD BROKEN AND FOULING ON A PIPE LOCATED ADJACENT TO THE AVM PICKUP. FAN BLADES CLEANED AND LUBRICATED AND AN ENGINE RUN CARRIED OUT.SDR AUS20021244Engine · vibrates(AUS) NR 4 ENGINE VIBRATION EXCESSIVE. ENGINE VIBRATION WAS ACCOMPANIEDBY A NOTICEABLE AIRFRAME VIBRATION.SDR AUS20021149Pump · failed(AUS) NR 2 ENGINE DRIVEN FUEL PUMP FAILED.SDR AUS20021065Engine · vibrates(AUS) NR 4 ENGINE VIBRATION CAUSED INFLIGHT SHUTDOWN.SDR AUS20021003Plate · leaking(AUS) NR 2 ENGINE HYDRAULIC PUMP BLANKING PLATE LEAKING ENGINE OIL. THE HYDRAULIC PUMP HAD BEEN REMOVED FROM THE ENGINE AND THE BLANKING PLATE FITTED.SDR AUS20020994Engine · failed(AUS) NR 1 ENGINE FAILED. EXCESSIVE VIBRATION INDICATIONS. INSPECTION FOUND METAL IN TAILPIPE.SDR AUS20020743Controller · faulty(AUS) NO1 ENGINE VIGV CONTROLLER FAULTY. CONTROLLER COULD NOT BE ADJUSTED TO BRING ENGINE PARAMETERS WITHIN LIMITS.SDR AUS20020606Pushrod · failed(AUS) FORWARD CARGO DOOR FAILED TO OPEN. A LOUD NOISE WAS HEARD AND SEVERAL PUSHRODS HAD SHEARED.SDR AUS20020406Engine · vibrates(AUS) DURING CLIMB NR 4 ENGINE VIBRATION INDICATED 2.0. ON B' SELECTION THE INDICATION WENT OFF SCALE WITH AVM ALERT FLASHING. PRIOR TO SHUTDOWN A SLIGHT AIRFRAME VIBRATION WAS FELT THROUGH THE AIRCRAFT.SDR AUS20020380Engine · failed(AUS) ON ROTATION A LOUD BANG WAS HEARD AND NR 4 EPR INDICATION DROPPED AND SPARKS WERE REPORTED FROM THE NR 4 ENGINE. THE ENGINE WAS SHUT DOWN.SDR AUS20020305Handle · out of adjust(AUS) L5 DOOR HANDLE RIGGING OUT OF ADJUSTMENT.SDR AUS20020281Hose · ruptured(AUS) NR 1 ADP PRESSURE HOSE LOCATED BETWEEN THE PUMP AND THE PRESSURE MODULE RUPTURED. LOSS OF HYDRAULIC FLUID.SDR AUS20020153Connector · loose(AUS) CAPTAINS NR 1 WINDOW HEAT CONNECTION LOCATED IN THE LOWER LT CORNER LOOSE AND ARCING.SDR AUS20020118Engine · stalled(AUS) NR 1 ENGINE STALLED. VIBRATION FELT AND ENGINE PARAMETERS DIFFERENT FROM OTHER ENGINES.SDR AUS20020094Coupling · separated(AUS) NR 6 AND NR 7 LEADING EDGE FLAPS DISCONNECTED DUE TO THE OUTBOARD SPLINE COUPLING COMING ADRIFT. THERE WAS NO SIGN OF THE LOCKWIREOR ATTACHMENT SCREWS.SDR AUS20020089Actuator · faulty(AUS) RUDDER RATIO ACTUATOR FAULTY.SDR AUS20020067Coupling · misrigged(AUS) FUEL TRANSFER SYSTEM COUPLING INCORRECTLY ASSEMBLED.SDR AUS20020032Control Unit · faulty(AUS) NR 2 ENGINE VIBRATION SIGNAL CONTROL UNIT SUSPECT FAULTY.SDR AUS20011437Bolt · sheared(AUS) H11 BOLT LOCATED AT STN 1241/LBBL 127/WL 163 SHEARED. FOLLOWING REMOVAL OF THE BOLT CORROSION WAS FOUND IN THE BULKHEAD FITTING BORE. FOUND DURING ULTRASONIC INSPECTION.SDR AUS20011381Bolt · loose(AUS) NR 1 ENGINE FUEL FLOW REGULATOR (FFR) TO FUEL PUMP PIPE LEAKING. INVESTIGATION FOUND A LOOSE PIPE RETAINING BOLT ON THE FFR.SDR AUS20011217Computer · failed(AUS) UPPER YAW DAMPER COMPUTER FAULTY.SDR AUS20011178Line · damaged(AUS) HYDRAULIC LINE DAMAGED BY CONTACT FROM THE RT WING LANDING GEAR RETRACTION ACTUATOR. LOSS OF NR 4 HYDRAULIC SYSTEM FLUID.SDR AUS20011132Control Cable · seized(AUS) NR 1 ENGINE THRUST LEVER PUSH/PULL CABLE SEIZED.SDR AUS20010980Engine · vibrates(AUS) NR 1 ENGINE VIBRATION. OIL QUANTITY SLOWLY DROPPED. METAL CONTAMINATION OF ENGINE OIL SYSTEM.SDR AUS20010949Connector · burned(AUS) SEAT 43AB VIDEO CONNECTOR PINS BURNT AND WIRING CHAFED.SDR AUS20010928Cover · cracked(AUS) LT AND RT ENGINE THRUST CABLE GUARD COVERS LOCATED IN AREABETWEEN BS960 TO BS1000 DETERIORATED AND CRACKED. FOUND DURING INSPECTION IAW EI 743-076-0002R02.SDR AUS20010910Actuator · sheared(AUS) NOSE LANDING GEAR DOOR ACTUATOR SHEARED. LOSS OF HYDRAULIC FLUID.SDR AUS20010911Pdu · faulty(AUS) NR 3 LT LEADING EDGE FLAP PNEUMATIC DRIVE UNIT FAULTY.SDR AUS20010883Engine · vibrates(AUS) NR 2 ENGINE VIBRATION EXCESSIVE.SDR AUS20010905Antenna · faulty(AUS) WEATHER RADAR ANTENNA FAULTY.SDR AUS20010839Fuel Control · faulty(AUS) NR 4 ENGINE FUEL FLOW REGULATOR FAULTY. AIRCRAFT IS FOREIGN REGISTRATION DQ-FJE.SDR AUS20010801Rotor · failed(AUS) NR 7 MAIN BODY WHEEL BRAKE ROTOR SEGMENT FAILED.
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